Books on the topic 'High speed rotor'
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Huppunen, Jussi. High-speed solid-rotor induction machine: Electromagnetic calculation and design. Lappeenranta: Lappeenranta University of Technology, 2004.
Find full textRutherford, John W. Shock fitting applied to the prediction of high-speed rotor noise. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1985.
Find full textJohnson, Wayne. Calculated performance, stability, and maneuverability of high-speed tilting-prop-rotor aircraft. [S.l.]: [s.n.], 1986.
Find full textJohnson, Wayne. Calculated performance, stability, and maneuverability of high-speed tilting-prop-rotor aircraft. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.
Find full textLance, Michael B. Low-speed wind-tunnel test of an unpowered high-speed stoppable rotor concept in fixed-wing mode. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.
Find full textY, Sung Daniel, Stroub Robert H, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Low-speed wind-tunnel test of an unpowered high-speed stoppable rotor concept in fixed-wing mode. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.
Find full textY, Sung Daniel, Stroub Robert H, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Low-speed wind-tunnel test of an unpowered high-speed stoppable rotor concept in fixed-wing mode. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.
Find full textLance, Michael B. Low-speed wind-tunnel test of an unpowered high-speed stoppable rotor concept in fixed-wing mode. Hampton, Va: Langley Research Center, 1991.
Find full textY, Sung Daniel, Stroub Robert H, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Low-speed wind-tunnel test of an unpowered high-speed stoppable rotor concept in fixed-wing mode. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.
Find full textUnited States. National Aeronautics and Space Administration., ed. Performance analysis of two early NACA high speed propellers with application to civil tiltrotor configurations. [Washington, DC]: National Aeronautics and Space Administration, 1996.
Find full textUnited States. National Aeronautics and Space Administration., ed. A new higher-order composite theory for analysis and design of high speed tilt-rotor blades. [Washington, D.C.]: National Aeronautics and Space Administration, 1996.
Find full textUnited States. National Aeronautics and Space Administration., ed. A new higher-order composite theory for analysis and design of high speed tilt-rotor blades. [Washington, D.C.]: National Aeronautics and Space Administration, 1996.
Find full textUnited States. Congress. Office of Technology Assessment., ed. New ways: Tiltrotor aircraft and magnetically levitated vehicles. Washington, DC: Congress of the U.S., Office of Technology Assessment, 1991.
Find full textR, McCarthy Thomas, and United States. National Aeronautics and Space Administration., eds. An integrated optimum design approach for high speed prop rotors: Final report on NASA Ames grant no. NCC2-795. [Washington, D.C: National Aeronautics and Space Administration, 1995.
Find full textChattopadhyay, Aditi. Optimum design of high speed prop-rotors. [Washington, DC: National Aeronautics and Space Administration, 1992.
Find full textUnited States. National Aeronautics and Space Administration., ed. Optimum design of high speed prop-rotors. [Washington, DC: National Aeronautics and Space Administration, 1992.
Find full textJ, Schneider J., Bartie K. M, and Ames Research Center, eds. Technology needs for high-speed rotorcraft (I). Philadelphia, PA: Boeing Helicopters, 1991.
Find full textCenter, Ames Research, and United States. Army Aviation Research and Technology Activity., eds. Wake model for helicopter rotors in high speed flight. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.
Find full textGahagan, Shane G. Pressure-sensitive paint measurements on a rotor disk surface at high speeds. Monterey, Calif: Naval Postgraduate School, 1997.
Find full textH, Goldthorpe Steve, and Langley Research Center, eds. Guidance and control requirements for high-speed rollout and turnoff (ROTO). Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
Find full textH, Goldthorpe S., and Langley Research Center, eds. Guidance and control design for high-speed rollout and turnoff (ROTO): Contract NAS1-19703. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.
Find full textG, Steenken W., and Hugh L. Dryden Flight Research Center., eds. Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1999.
Find full textVaez-Zadeh, Sadegh. Rotor Position and Speed Estimation. Oxford University Press, 2018. http://dx.doi.org/10.1093/oso/9780198742968.003.0006.
Full textNational Aeronautics and Space Administration (NASA) Staff. Low-Speed Wind-Tunnel Test of an Unpowered High-Speed Stoppable Rotor Concept in Fixed-Wing Mode. Independently Published, 2018.
Find full textPerformance analysis of two early NACA high speed propellers with application to civil tiltrotor configurations. [Washington, DC]: National Aeronautics and Space Administration, 1996.
Find full textA new higher-order composite theory for analysis and design of high speed tilt-rotor blades. [Washington, D.C.]: National Aeronautics and Space Administration, 1996.
Find full textA new higher-order composite theory for analysis and design of high speed tilt-rotor blades. [Washington, D.C.]: National Aeronautics and Space Administration, 1996.
Find full textWindage Power Loss in Gas Foil Bearings and the Rotor-Stator Clearance of High Speed Generators Operating in High Pressure Environments. Independently Published, 2019.
Find full textCost characteristics of tilt-rotor, conventional air and high speed rail short-haul intercity passenger service: Final report. Moffett Field, CA: Powered Lift Flight Investigation Branch, National Aeronautics and Space Administration, Ames Research Center, 1985.
Find full textCost characteristics of tilt-rotor, conventional air and high speed rail short-haul intercity passenger service: Final report. Moffett Field, CA: Powered Lift Flight Investigation Branch, National Aeronautics and Space Administration, Ames Research Center, 1985.
Find full textNational Aeronautics and Space Administration (NASA) Staff. Optimum Design of High-Speed Prop-Rotors. Independently Published, 2018.
Find full textPressure-Sensitive Paint Measurements on a Rotor Disk Surface at High Speeds. Storming Media, 1997.
Find full textGuidance and control requirements for high-speed rollout and turnoff (ROTO). Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
Find full textThe selection of convertible engines with current gas generator technology for high speed rotorcraft. [Washington, DC]: National Aeronautics and Space Administration, 1991.
Find full textNational Aeronautics and Space Administration (NASA) Staff. Optimum Design of High Speed Prop Rotors Including the Coupling of Performance, Aeroelastic Stability and Structures. Independently Published, 2018.
Find full textAn integrated optimum design approach for high speed prop rotors: Final report on NASA Ames grant no. NCC2-795. [Washington, D.C: National Aeronautics and Space Administration, 1995.
Find full textAn Integrated optimum design approach for high speed prop-rotors including acoustic constraints: Semi-annual progress report ... January 1 - June 30, 1993. [Washington, DC: National Aeronautics and Space Administration, 1993.
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